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Aircraft Design -
an Open Educational Resource (OER)
for Hamburg Open Online University (HOOU)

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Videos about Aircraft Design and this OER

Aircraft Design @ HOOU - Teaser
German, English subtitles (2016)

Aircraft Design @ HOOU - Introduction

Aircraft Design @ HOOU - Interview
Prof. Scholz, German (2016)

Aircraft Design @ HOOU - Interview
Prof. Scholz, English (2016)

Subtitles? Start video, click on "YouTube", switch on Subtitles and switch to English Language there!



This OER in a Graphics-Based Version pin
This OER at HOOU
Background of HOOU and this OER


Start to Learn with this Hotspot Picture

Get started with Aircraft Design by learning about the main parts of an aircraft.
Click on (+) to get a Definition of the related aircraft component and follow the links to Wikipedia and NASA to learn more.
Click on the Hotspot (+) which is up in the air in the picture for an Introduction!!!
Look at NASA's Overview of Aircraft Parts.
The picture shows an Emirates Airbus A340-300 (source).


Lecture Notes

Since 2017-03-24 almost all PDF-files are password protection due to actual, possible, or perceived copyright issues. User: student. PW: ?

Dieter SCHOLZ: Aircraft Design
Chapter Titel Number of Pages PDF Remarks
  Title Page 2 *.pdf Available without password.
  Contents 4 *.pdf Available without password.
1 Introduction 7 *.pdf  
2 Aircraft Design Sequence 6 *.pdf  
3 Requirements and Certification 6 *.pdf  
4 Aircraft Configurations 11 *.pdf  
5 Preliminary Sizing 32 *.pdf  
6 Fuselage Design 21 *.pdf  
7 Wing Design 43 *.pdf  
8 High Lift Systems and Maximum Lift Coefficients 21 *.pdf  
9 Empennage General Design 16 *.pdf  
10 Mass and Center of Gravity 24 *.pdf  
11 Empennage Sizing 29 *.pdf  
12 Landing Gear Conceptual Design and Integration 13 *.pdf Author: Bernd Trahmer.
13 Drag Prediction 16 *.pdf  
14 Design Evaluation / DOC 32 *.pdf  
  References 3 *.pdf Available without password.
  Sum: 286    
Appendix A Estimating the Oswald Factor from Basic Aircraft Geometrical Parameter 35 *.pdf One step to a realistic drag polar (induced drag). Available without password.
Appendix B Calculation of Wave Drag, Relative Wing Thickness, Fuselage Nose Length 12 *.pdf Another step to a realistic drag polar (wave drag), estimating relative wing thickness, and fuselage nose length. Available without password.
  Sum, Appendix: 47    
Summary Aircraft Design in a Nutshell 25 *.pdf Please make much use of this file to get prepared for the examination. Available without password.
Examination Examination in the Short Course Aircraft Design 5 *.pdf Available without password.
Solution Solution for the Examination in the Short Course Aircraft Design 19 *.pdf Please check your own results based on what is written here. Available without password.

Please see the Aircraft Design page with "official pictures" of teams taking this OER as a short course.


Aircraft Design Videos in my Playlists on YouTube

Test Your Aircraft Design Knowledge

Author: Dieter Scholz

STAND:  19 April 2017
AUTHOR:  Prof. Dr. Scholz
home  Prof. Dr. Scholz
home  Aircraft Design and Systems Group (AERO)
home  Aeronautical Engineering   deutsch
home  Department of Automotive and Aeronautical Engineering  deutsch
home  Faculty of Engineering and Computer Science
home  Hamburg University of Applied Sciences